Paper
6 April 1988 Light-Weight Electrochemical Converter For Space Power Applications
Michael Hsu
Author Affiliations +
Proceedings Volume 0871, Space Structures, Power, and Power Conditioning; (1988) https://doi.org/10.1117/12.943634
Event: 1988 Los Angeles Symposium: O-E/LASE '88, 1988, Los Angeles, CA, United States
Abstract
An innovative concept for space power systems utilizes an electrochemical-loop, which comprises a high temperature electrolytic cell and a low temperature fuel cell. In the electrolytic cell, the working fluid is electrolyzed using combined thermal and electrical input. The products of the electrolysis are recombined in a lower temperature fuel cell, generating more voltage output than required to operate the electrolytic cell. The excess electricity from the loop is available for external loads. The thermal energy can be made available from a nuclear reactor. The zirconia cells of solid oxide electrolyte under development by Ztek would serve as the high temperature electrolytic cell. The low temperature fuel cells, which are under development in various space programs, can be adapted for this system. Studies suggest that this system is a desirable light-weight option in meeting future space power needs. Recent technical advances in zirconia cell development have brought the hardware loop integration close to realization.
© (1988) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Michael Hsu "Light-Weight Electrochemical Converter For Space Power Applications", Proc. SPIE 0871, Space Structures, Power, and Power Conditioning, (6 April 1988); https://doi.org/10.1117/12.943634
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KEYWORDS
Zirconium dioxide

Silver

Carbonates

Solar energy

Thermoelectric materials

Space operations

Amplifiers

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